TM 1-1520-240-MTF2-85IN-FLIGHT (CONT.) (5) Accomplish Power Recovery prior to1000’ AGL.(a)Load Rotor by relaxing pressure onThrust Control Lever allowing it tocome up as required if RRPM isabove 100%.(b)FADEC NR% rheostat — 100%position.(c)Reestablish 100% RRPM, safeairspeed, and altitude.(d)Climb back to altitude where PAwas noted and record following:1 Free Air Temperature.2 Fuel Quantity.(e)Record previously noted: RRPM.PA, Pedal Separation, andUnusual Vibrations (as applicable).(6) Compare data to chart in Section V forproper RRPM. Ensure conversion fromPA and FAT to DA.13. 712 Engine TEAC check, if required. (Refer toSection IV.)14. 714A Power Assurance Check, if required.(Refer to Section IV.)15. Fuel consumption check — STOP.16. Navigation and Communication. (Refer toSection IV.)17. Miscellaneous (as required).a. Vertical velocity indicatorsb. Turn and slip indicators.
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